Federal Register / Vol. 77, No. 230 / Thursday, November 29, 2012 / Rules and Regulations 71085 

Federal Reserve Board’s’’ between the 

words ‘‘to’’ and ‘‘Regulation.’’; and 

■ c. In the note to sample form B–5 by 

removing ‘‘12 CFR 202.4(c)(2)’’ and 

adding in its place ‘‘12 CFR 204.2(c)(2)’’. 

Appendix C to Part 707 [Amended] 

■ 8. Amend appendix C to part 707 as 

follows: 

■ a. In the entry for section 707.2, under 

‘‘(a),’’ paragraph 5 v by removing ‘‘12 

CFR 230.2(u)’’ and adding in its place 

‘‘12 CFR 1030.2(u)’’ and adding to the 

last sentence the words ‘‘Federal 

Reserve Board’s’’ between the words 

‘‘in’’ and ‘‘Regulation D’’; 

■ b. In the entry for section 707.2, under 

‘‘(s),’’ paragraph 1 by removing ‘‘12 CFR 

205.2(j)’’ and adding in its place ‘‘12 

CFR 1005.2(k)’’; 

■ c. In the entry for section 707.2, under 

‘‘(x),’’ paragraph 1 heading by adding 

the words ‘‘the Federal Reserve Board’s’’ 

before the words ‘‘Regulation D’’ and 

adding in the first sentence of this 

section the words ‘‘The Federal Reserve 

Board’s’’ before the words ‘‘Regulation 

D permits,’’; 

■ d. in the entry for section 707.3, under 

‘‘(c),’’ paragraph 1 introductory text by 

removing ‘‘12 CFR part 205’’ and adding 

in its place ‘‘12 CFR part 1005’’; 

■ e. In the entry for section 707.3, under 

‘‘(c),’’ paragraph 1 ii by removing ‘‘12 

CFR 205.7’’ and adding in its place ‘‘12 

CFR 1005.7’’; 

■ f. In the entry for section 707.4, under 

‘‘(b)(4),’’ paragraph 5 by removing ‘‘12 

CFR 205.7’’ and adding in its place ‘‘12 

CFR 1005.7’’; 

■ g. In the entry for section 707.6, under 

‘‘(a),’’ paragraph 2 by removing ‘‘12 CFR 

205.9’’ and adding in its place ‘‘12 CFR 

1005.9’’; 

■ h. In the entry for section 707.8, under 

‘‘(a),’’ paragraph 10 i by removing ‘‘12 

CFR part 226’’ and adding in its place 

‘‘12 CFR part 1026’’; 

■ i. In the entry for section 707.11, 

under ‘‘(a)(1),’’ paragraph 1 1 i by 

removing ‘‘12 CFR part 226’’ and adding 

in its place ‘‘12 CFR part 1026’’; 

■ j. In the entry for section 707.11, 

under ‘‘(a)(1),’’ paragraph 2 by removing 

the words ‘‘the Federal Reserve Board’s’’ 

and removing ‘‘12 CFR part 226’’ and 

adding in its place ‘‘12 CFR part 1026’’; 

■ k. In the entry for section 707.11, 

under ‘‘(b),’’ paragraph 1 i by removing 

‘‘12 CFR part 226’’ and adding in its 

place ‘‘12 CFR part 1026’’; 

■ l. In the entry for section 707.11, 

under ‘‘(b)’’ paragraph 4 by removing 

‘‘12 CFR part 226’’ and adding in its 

place ‘‘12 CFR part 1026’’; 

■ m. In the entry for section 707.11, 

under ‘‘(c),’’ paragraph 1 by removing 

the words ‘‘part 226’’ and adding in its 

place the words ‘‘part 1026’’; and 

■ n. In the entry for section 707.11, 

under ‘‘(c),’’ by removing in two places 

in paragraph 3 ‘‘12 CFR part 226’’ and 

adding in its place ‘‘12 CFR part 1026’’ 

and by removing in two place in 

paragraph 3 the phrase ‘‘the Federal 

Reserve Board’s’’ before the words 

‘‘Regulation Z’’. 

PART 714—LEASING 

■ 9. The authority citation for part 714 

continues to read as follows: 

Authority: 12 U.S.C. 1756, 1757, 1766, 

1785, 1789. 

§ 714.10 [Amended] 

■ 10. Amend § 714.10 by removing ‘‘12 

CFR part 213’’ and adding in its place 

‘‘12 CFR part 1013’’. 

PART 748—SECURITY PROGRAM, 

REPORT OF SUSPECTED CRIMES, 

SUSPICIOUS TRANSACTIONS, 

CATASTROPHIC ACTS AND BANK 

SECRECY ACT COMPLIANCE 

■ 11. The authority citation for part 748 

is revised to read as follows: 

Authority: 12 U.S.C. 1766(a), 1786(q); 15 

U.S.C. 6801–6809; 31 U.S.C. 5311 and 5318. 

Appendix A to Part 748 [Amended] 

■ 12. Amend appendix A to part 748 by 

removing paragraph III.G. 

PART 749—RECORDS 

PRESERVATION PROGRAM AND 

APPENDICES—RECORD RETENTION 

GUIDELINES; CATASTROPHIC ACT 

PREPAREDNESS GUIDELINES 

■ 13. The authority citation for part 749 

continues to read as follows: 

Authority: 12 U.S.C. 1766, 1783, and 1789; 

15 U.S.C. 7001(d). 

Appendix A to Part 749 [Amended] 

■ 14. Amend appendix A to part 749 by 

removing paragraph E.1.(c). 

[FR Doc. 2012–28666 Filed 11–28–12; 8:45 am] 

BILLING CODE 7535–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1056; Directorate 

Identifier 2012–NE–32–AD; Amendment 39– 

17271; AD 2012–24–01] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

Deutschland Ltd & Co KG Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

serial number (S/N) Rolls-Royce 

Deutschland Ltd & Co KG (RRD) TAY 

620–15 turbofan engines. This AD 

requires initial and repetitive general 

inspections and ultrasonic inspections 

(UI) of low-pressure compressor (LPC) 

fan blades for cracks. If any fan blade is 

found cracked, this AD requires 

replacement of the LPC fan blade set 

and the LPC fan disc. This AD was 

prompted by a report of an LPC fan 

blade separation. We are issuing this AD 

to detect cracks in the LPC fan blades, 

which could lead to uncontained failure 

of the LPC fan blades and LPC fan disc, 

and damage to the airplane. 

DATES: This AD becomes effective 

December 14, 2012. 

We must receive comments on this 

AD by January 14, 2013. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov and follow 

the instructions for sending your 

comments electronically. 

• Mail: U.S. Department of 

Transportation, 1200 New Jersey 

Avenue SE., West Building Ground 

Floor, Room W12–140, Washington, DC 

20590–0001. 

• Hand Delivery: Deliver to Mail 

address above between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

• Fax: 202–493–2251. 

For service information identified in 

this AD, contact Rolls-Royce 

Deutschland Ltd & Co KG, Eschenweg 

11, Dahlewitz, 15827 BlankenfeldeMahlow, Germany; phone: 49 0 33– 

7086–1944; fax: 49 0 33–7086–3276. 

You may view this service information 

at the FAA, Engine & Propeller 

Directorate, 12 New England Executive 

Park, Burlington, MA 01803. For 

information on the availability of this 

material at the FAA, call 781–238–7125. 


pmangrum on DSK3VPTVN1PROD with RULES
71086 Federal Register / Vol. 77, No. 230 / Thursday, November 29, 2012 / Rules and Regulations 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; or in person at the 

Docket Operations office between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Operations office (phone: 

800–647–5527) is the same as the Mail 

address provided in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Frederick Zink, Aerospace Engineer, 

Engine Certification Office, FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

phone: 781–238–7779; fax: 781–238– 

7199; email: Frederick.zink@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Community, has issued EASA 

Airworthiness Directive 2012–0185–E, 

dated September 12, 2012 (referred to 

after this as ‘‘the MCAI’’), to correct an 

unsafe condition for the specified 

products. The MCAI states: 

Fan blade off on a TAY 620–15 engine has 

recently been reported. Subsequent 

investigation results identified vibration 

induced by a fan blade flutter as a possible 

cause of fan blade root failure leading to 

blade off. 

This condition, if not detected and 

corrected, could lead to the blade failure 

potentially causing release of high-energy 

debris, possibly resulting in damage to the 

aeroplane and/or injury to the occupants. 

You may obtain further information by 

examining the MCAI in the AD docket. 

FAA’s Determination and Requirements 

of This AD 

This product has been approved by 

EASA, and is approved for operation in 

the United States. Pursuant to our 

bilateral agreement with the European 

Community, EASA has notified us of 

the unsafe condition described in the 

MCAI and service information 

referenced above. We are issuing this 

AD because we evaluated all 

information provided by EASA and 

determined the unsafe condition exists 

and is likely to exist or develop on other 

products of the same type design. This 

AD requires initial and repetitive 

general inspections and UIs of LPC fan 

blades for cracks. If any fan blade is 

found cracked, this AD requires 

replacement of the LPC fan blade set 

and the LPC fan disc. 

FAA’s Determination of the Effective 

Date 

No domestic operators use this 

product. Therefore, we find that notice 

and opportunity for prior public 

comment are unnecessary and that good 

cause exists for making this amendment 

effective in less than 30 days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety and 

was not preceded by notice and an 

opportunity for public comment. 

However, we invite you to send any 

written data, views, or arguments about 

this AD. Send your comments to an 

address listed under the ADDRESSES

section. Include the docket number 

FAA–2012–1056 and Directorate 

Identifier 2012–NE–32–AD at the 

beginning of your comments. We 

specifically invite comments on the 

overall regulatory, economic, 

environmental, and energy aspects of 

this AD. We will consider all comments 

received by the closing date and may 

amend this AD because of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

about this AD. Using the search function 

of the Web site, anyone can find and 

read the comments in any of our 

dockets, including, if provided, the 

name of the individual who sent the 

comment (or signed the comment on 

behalf of an association, business, labor 

union, etc.). You may review the DOT’s 

complete Privacy Act Statement in the 

Federal Register published on April 11, 

2000 (65 FR 19477–78). 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

section 106, describes the authority of 

the FAA Administrator. ‘‘Subtitle VII: 

Aviation Programs,’’ describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in ‘‘Subtitle VII, 

Part A, Subpart III, Section 44701: 

General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We determined that this AD will not 

have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify this AD: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); and 

3. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new AD: 

2012–24–01 Rolls-Royce Deutschland Ltd & 

Co KG (formerly Rolls-Royce plc): 

Amendment 39–17271; Docket No. 

FAA–2012–1056; Directorate Identifier 

2012–NE–32–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective December 14, 2012. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Rolls-Royce 

Deutschland Ltd & Co KG (RRD) TAY 620– 

15 engines, serial numbers 17054, 17085, 

17088, 17107, and 17166. 


pmangrum on DSK3VPTVN1PROD with RULES
Federal Register / Vol. 77, No. 230 / Thursday, November 29, 2012 / Rules and Regulations 71087 

(d) Reason 

This AD was prompted by a report of a 

low-pressure compressor (LPC) fan blade 

separation. We are issuing this AD to detect 

cracks in the LPC fan blades, which could 

lead to uncontained failure of the LPC fan 

blades and LPC fan disc, and damage to the 

airplane. 

(e) Actions and Compliance 

Unless already done, do the following 

actions: 

(1) Before further flight after the effective 

date of this AD, perform a visual inspection 

and ultrasonic inspection of the LPC fan 

blades to determine general condition and/or 

the presence of cracks. 

(2) Thereafter, perform the inspections 

specified in paragraph (e)(1) of this AD 

within every additional 1,500 flight hours 

(FHs), but not fewer than 1,000 FHs. 

(3) If any fan blade is found cracked, 

replace the LPC fan blade set and the LPC fan 

disc before further flight. 

(f) Terminating Action 

Replacing the LPC fan blade set and the 

LPC fan disc is terminating action to the 

repetitive inspections required by this AD. 

(g) Alternative Methods of Compliance 

(AMOCs) 

The Manager, Engine Certification Office, 

FAA, may approve AMOCs to this AD. Use 

the procedures found in 14 CFR 39.19 to 

make your request. 

(h) Related Information 

(1) For more information about this AD, 

contact Frederick Zink, Aerospace Engineer, 

Engine Certification Office, FAA, Engine & 

Propeller Directorate, 12 New England 

Executive Park, Burlington, MA 01803; 

email: Frederick.zink@faa.gov; phone: 781– 

238–7779; fax: 781–238–7199. 

(2) Refer to European Aviation Safety 

Agency AD 2012–0185–E, dated September 

12, 2012, and RRD Alert Service Bulletin 

TAY–72–A1775, Revision 1, dated 

September 12, 2012, for related information. 

(3) For service information identified in 

this AD, contact Rolls-Royce Deutschland Ltd 

& Co KG, Eschenweg 11, Dahlewitz, 15827 

Blankenfelde-Mahlow, Germany; telephone: 

49 0 33–7086–1944; fax: 49 0 33–7086–3276. 

(4) You may view this service information 

at the FAA, Engine & Propeller Directorate, 

12 New England Executive Park, Burlington, 

MA. For information on the availability of 

this material at the FAA, call 781–238–7125. 

(i) Material Incorporated by Reference 

None. 

Issued in Burlington, Massachusetts, on 

November 19, 2012. 

Robert J. Ganley, 

Acting Manager, Engine & Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–28638 Filed 11–28–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1206; Directorate 

Identifier 2012–SW–021–AD; Amendment 

39–17269; AD 2012–23–13] 

RIN 2120–AA64 

Airworthiness Directives; Sikorsky 

Aircraft Corporation (Sikorsky) Model 

Helicopters 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for 

Sikorsky Model S–70, S–70A, and S– 

70C helicopters, which are restricted 

category helicopters derived from the 

military Model UH–60 helicopter. This 

AD would require reducing or 

establishing life limits for certain listed 

helicopter parts. This AD is prompted 

by a review of the United States Army’s 

analysis of their Model UH–60 fleet, 

which determined it necessary to 

establish or reduce the life limits of 

certain parts. The actions are intended 

to prevent fatigue failure of a part and 

subsequent loss of control of the 

helicopter. 

DATES: This AD becomes effective 

December 14, 2012. 

We must receive comments on this 

AD by January 28, 2013. 

ADDRESSES: You may send comments by 

any of the following methods: 

• Federal eRulemaking Docket: Go to 

http://www.regulations.gov. Follow the 

online instructions for sending your 

comments electronically. 

• Fax: 202–493–2251. 

• Mail: Send comments to the U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC 20590–0001. 

• Hand Delivery: Deliver to the 

‘‘Mail’’ address between 9 a.m. and 5 

p.m., Monday through Friday, except 

Federal holidays. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov or in person at the 

Docket Operations Office between 9 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. The AD 

docket contains this AD, the economic 

evaluation, any comments received, and 

other information. The street address for 

the Docket Operations Office (telephone 

800–647–5527) is in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

FOR FURTHER INFORMATION CONTACT: 

Michael Davison, Flight Test Engineer, 

New England Regional Office, FAA, 12 

New England Executive Park, 

Burlington, MA 01803; phone: (781) 

238–7156, email: 

michael.davison@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not provide you with notice and 

an opportunity to provide your 

comments prior to it becoming effective. 

However, we invite you to participate in 

this rulemaking by submitting written 

comments, data, or views. We also 

invite comments relating to the 

economic, environmental, energy, or 

federalism impacts that resulted from 

adopting this AD. The most helpful 

comments reference a specific portion of 

the AD, explain the reason for any 

recommended change, and include 

supporting data. To ensure the docket 

does not contain duplicate comments, 

commenters should send only one copy 

of written comments, or if comments are 

filed electronically, commenters should 

submit them only one time. We will file 

in the docket all comments that we 

receive, as well as a report summarizing 

each substantive public contact with 

FAA personnel concerning this 

rulemaking during the comment period. 

We will consider all the comments we 

receive and may conduct additional 

rulemaking based on those comments. 

Discussion 

We are adopting a new AD for 

Sikorsky Model S–70, S–70A and S–70C 

helicopters. This AD requires reducing 

or establishing life limits for the main 

rotor blade, tail rotor blade, planetary 

carrier assembly, tail rotor servo, 

elastomeric sleeve bearing, main 

landing gear shock strut piston cylinder, 

crossfeed valve, oil cooler axial fan ball 

bearing assembly, dowel pins, main 

rotor hub, and right tie rod attach bolt. 

This AD is prompted by the need to 

reduce life limits on the specified parts. 

This determination is based on a review 

of analysis by the U.S. Army of certain 

parts installed on the military Model 

UH–60 helicopters, which shows that 

the life limits of those parts need to be 

reduced. The Sikorsky Model S–70, S– 

70A and S–70C helicopters are 

restricted category helicopters derived 

from the military Model UH–60 

helicopter. The actions are intended to 


pmangrum on DSK3VPTVN1PROD with RULES